Purpose of study is to show application of perturbation technique in study of random response of multidegree-of-freedom nonlinear system simulating airplane moving with constant velocity along runway whose profile is represented by stationary random process; using pertinent characteristics of supersonic civil transport being designed in United States, numerical results are produced for response of simplified idealization of airplane; applicable to evaluation of fatigue damage of landing gear system and structural damage of airframe due to runway roughness.


    Access

    Download

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Effects of runway roughness on dynamic response of airplanes


    Additional title:

    J Sound Vibration


    Contributors:
    Tung, C.C. (author)

    Published in:

    Publication date :

    1967


    Size :

    9 pages



    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English


    Keywords :





    Runway Roughness Criteria

    Filarski, J. D. / American Society of Civil Engineers | British Library Conference Proceedings | 2001


    Runway roughness effects on new aircraft types

    Lee, H.R. / Scheffel, J.L. | Engineering Index Backfile | 1968